EP0701653B1 - Large two-stroke internal combustion engine with slide valve - Google Patents

Large two-stroke internal combustion engine with slide valve Download PDF

Info

Publication number
EP0701653B1
EP0701653B1 EP94902643A EP94902643A EP0701653B1 EP 0701653 B1 EP0701653 B1 EP 0701653B1 EP 94902643 A EP94902643 A EP 94902643A EP 94902643 A EP94902643 A EP 94902643A EP 0701653 B1 EP0701653 B1 EP 0701653B1
Authority
EP
European Patent Office
Prior art keywords
spool
movable part
pilot
bore
internal combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP94902643A
Other languages
German (de)
French (fr)
Other versions
EP0701653A1 (en
Inventor
Henning Lindquist
Erik Rosenlund Hansen
Karel Hampejs
Stefan Gabriel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN B&W Diesel GmbH
MAN B&W Diesel AS
Original Assignee
MAN B&W Diesel GmbH
MAN B&W Diesel AS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MAN B&W Diesel GmbH, MAN B&W Diesel AS filed Critical MAN B&W Diesel GmbH
Publication of EP0701653A1 publication Critical patent/EP0701653A1/en
Application granted granted Critical
Publication of EP0701653B1 publication Critical patent/EP0701653B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/44—Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • F02M59/46—Valves
    • F02M59/466—Electrically operated valves, e.g. using electromagnetic or piezoelectric operating means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L9/00—Valve-gear or valve arrangements actuated non-mechanically
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L9/00—Valve-gear or valve arrangements actuated non-mechanically
    • F01L9/10—Valve-gear or valve arrangements actuated non-mechanically by fluid means, e.g. hydraulic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
    • F02D1/12—Transmission of control impulse to pump control, e.g. with power drive or power assistance non-mechanical, e.g. hydraulic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
    • F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
    • F02M59/105—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive hydraulic drive
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/20—Varying fuel delivery in quantity or timing
    • F02M59/36—Varying fuel delivery in quantity or timing by variably-timed valves controlling fuel passages to pumping elements or overflow passages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S251/00—Valves and valve actuation
    • Y10S251/905—Movable coil electrical actuator, e.g. voice coil
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/86493—Multi-way valve unit
    • Y10T137/86574—Supply and exhaust
    • Y10T137/86582—Pilot-actuated
    • Y10T137/86614—Electric

Definitions

  • the invention relates to a large two-stroke internal combustion engine, such as a main engine of a ship, having at least one hydraulically driven cylinder member, particularly a fuel pump, in which the hydraulic drive of the member comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with a spool valve, the spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the spool is positionable by means of a positioning means electrically activated by a control unit which determines how the cylinder member is to be activated during an engine cycle and from this determines intended positions for the spool, and in which the positioning means includes a linear drive with a movable part which is displaceable in the longitudinal direction of the spool over a distance corresponding to the distance between the extreme positions of the spool.
  • An engine with such a spool valve is known from W089/03939 but there the movable part is axially positionally locked to the spool, and the positioning means has to move the whole mass of the spool.
  • the linear drive with the movable part is made as a hydraulic cylinder in which the movable piston is axially fixed to the spool. This movable member can influence the spool with very large axially directed forces, but is slow-acting.
  • EP-A 0 570 646 was published in November 1993, after the priority date of the present invention.
  • the document describes an internal combustion engine having a hydraulically driven fuel pump, in which the hydraulic drive comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with a spool valve, the first spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the first spool is positionable by means of a positioning means electrically activated to control the fuel pump, and in which the positioning means includes a linear drive with a movable part which is displaceable in the longitudinal direction of the spool, and in which the movable part carries windings positioned in a magnetic field, and in which the movable part is connected with a second spool that is axially displaceable, and in which a sensor detects the position of the first spool.
  • the first spool is moved proportionally to the movements of the second spool, the second spool can only be moved short distances, it has a relatively large mass, it is positionally suspended between mechanical springs, and there is no position feed-back to a control unit.
  • the object of the invention is to provide a large two-stroke internal combustion engine with a hydraulic drive which is quick-acting and may be set accurately, and at the same time is of a simple design.
  • the engine according to the invention being characterized in that the movable part carries windings positioned in a magnetic field in a slit which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings, that the movable part is connected with a small pilot spool which is axially displaceable with respect to the spool, that a sensor signals the actual position of the movable part to the control unit, that the spool follows the movements of the pilot spool, and that the control unit supplies current to the windings, if the actual position of the movable part differs from the intended position.
  • the hydraulic drive for the fuel pump can control initiation and termination of the fuel injection at exactly the desired moment of the engine cycle and with delivery of an accurately metered amount of oil.
  • the accurate control of the fuel injection renders it possible to reduce the specific fuel oil consumption of the engine, and further, the fuel injection may be divided into a pre-injection and a main injection merely by starting and stopping the hydraulic drive several times during a relatively small angle of rotation of the crankshaft.
  • the mass of the positioning means has been made so small that the setting speed is substantially determined by the mass to be moved by the positioning means.
  • the pilot spool may, for example, be designed with a mass of 10 g, which, for example, makes possible a spool move of 15 mm in 3-4 ms. This by far exceeds the setting speed obtainable so far for relatively large spool valves controlling high-pressure hydraulic drives.
  • the possibility of rapidly opening the spool valve for supply of large amounts of oil, and corresponding rapid resetting of the spool valve for relief of the pressure in the hydraulic cylinder renders possible a very fine control of the pressure on the delivery side of the hydraulic drive.
  • control unit may continuously monitor whether the spool is in the desired position. If the spool changes position owing to external influences, the control unit may immediately pass a corrective flash of current through the windings so that the actual position is made to correspond with the intended position.
  • the current intensity required for the position setting depends on the strength of the magnetic field in the oblong slit.
  • the side walls of the slit are delimited by an annular magnet and an iron-based material, respectively, as this in a simple manner produces a strong and uniform magnetic field which renders it possible to limit the size of the windings, in order that the already small mass of the movable part is reduced as much as possible, which promotes a rapid setting of the spool valve.
  • the movable part is in controlling connection with the spool via a rod extending coaxially with the spool and upon which the movable part is rigidly mounted.
  • the pilot spool functions by controlling control edges for high-pressure and low-pressure oil sources which may affect pressure faces in the spool.
  • the internal combustion engine is characterized in that at its first end the spool has an axially extending bore which communicates with the high-pressure source, and in which a piston supported by the spool housing is displaceably inserted in a tightly fitting manner, that at its second end the spool has an axially extending bore in which a piston supported by the spool housing is displaceably inserted in a tightly fitting manner, that the bore at the second end of the spool has a conduit extending to the pilot spool and having a mouth which may be barred by the flange of the pilot spool, and that the bore at the second end of the spool has a larger cross sectional area than the bore at the first end of the spool.
  • the high-pressure connection to the smallest bore at the first end of the spool causes a permanent force on the spool acting in a direction towards the second end of the spool. If this force displaces the spool in relation to the pilot spool, the conduit mouth is opened at the pilot spool flange to the high-pressure source, so that the pressure in the large bore at the second end of the spool is increased, whereby a force directed towards the first end of the spool increases, so that the spool again occupies a neutral position in relation to the pilot spool, in which position the two oppositely directed forces balance.
  • the spool is displaced so that the conduit mouth is brought into contact with the low-pressure port, thus relieving the pressure in the large bore to the level of balance.
  • the setting speed of the spool in relation to the pilot spool may be freely selected by adapting the mutual cross sectional area between the large and the small bore at either end of the spool.
  • the pilot spool can be positioned inside the spool, preferably coaxially with it, and may have two circumferential grooves in its peripheral surface and a flange positioned between the grooves, which two grooves of the pilot spool communicate with the high-pressure source and the low-pressure port, respectively.
  • the present invention also relates to a spool valve for control of a hydraulic drive, such as a drive for a fuel pump or an exhaust valve of an internal combustion engine, in which the hydraulic drive comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with the spool valve, the spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the spool is positionable by means of a positioning means electrically activated by a control unit, and in which the positioning means has a movable part and a sensor signalizing the actual position of the movable part to the control unit which determines intended positions for the spool and for a movable part.
  • a hydraulic drive such as a drive for a fuel pump or an exhaust valve of an internal combustion engine
  • the hydraulic drive comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in
  • This spool valve is characterized in that the movable part carries windings positioned in a magnetic field in a slit which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings, that the movable part is connected with a small pilot spool which is axially displaceable with respect to the spool, that the spool follows the movements of the pilot spool, that the control unit supplies current to the windings, if the actual position of the movable part differs from the intended position, that at its first end the spool has an axially extending bore which communicates with the high-pressure source, and in which a piston supported by the spool housing is displaceably inserted, that at its second end the spool has an axially extending bore in which a piston supported by the spool housing is displaceably inserted, that the bore at the second end of the
  • the positioning means is designed as a linear motor with movable windings and with positioning feedback to the control unit.
  • the spool follow the movements of the movable part with the pilot spool an unambiguous and well-defined coherence between the control of the positioning means and the control of the hydraulic drive is obtained in a simple manner.
  • From the driving unit of a loudspeaker it is known to use a movable part with windings positioned in a magnetic field in an oblong slit. In the loudspeaker, the windings are fed with an alternating voltage of a frequency which causes a corresponding oscillation frequency in the membrane connected with the movable part.
  • the movable part may perform even extremely rapid setting movements.
  • the control unit may cause very rapid movements in the part and the associated spool.
  • the maximum travel of the movable part may be freely selected according to need by designing the oblong slit with a larger length than the largest travel desired from the movable part.
  • the movable part only moves when current passes through the windings, and the desired direction, magnitude and speed of the movement may be freely selected by adaptation of the current intensity and the current direction of the windings.
  • the movable part may thus rapidly be started and stopped immediately at any desired intermediate position between the extreme positions.
  • Fig. 1 shows a large two-stroke diesel engine of the crosshead type generally designated 1, which may be used as the main engine of a ship or as a stationary power-producing engine.
  • the combustion chamber 2 of the engine is delimited by a cylinder liner 3 and a cylinder cover 4 and a piston 5 journalled in the liner.
  • a piston rod 6 Via a piston rod 6, the piston is directly connected with a crosshead 7 which, via a connecting rod 8, is directly connected with a connecting rod pin 9 in a throw 10 of a crankshaft 11.
  • a cylinder member in the form of an exhaust valve 12 with associated housing 13 is mounted on the cover 4. The exhaust valve is activated by a hydraulic drive 14 controlled by an electro-mechanical spool valve activated by control signals transmitted through a wire 15 from a computer 16.
  • a fuel valve 17 mounted in the cover 4 may supply atomized fuel to the combustion chamber 2.
  • Another cylinder member in the form of a fuel pump 18 is controlled by an electro-mechanical spool valve and may supply fuel to the fuel valve through a pressure line 19 in dependency of control signals received from the computer 16 through a wire 20.
  • the computer 16 is supplied with information on the actual number of revolutions per minute of the engine. The number of revolutions may either be taken from the tachometer of the engine, or it may originate from an angle detector and indicator mounted on the main shaft of the engine and determining the actual angular position and rotating speed of the engine for intervals constituting fractions of an engine cycle of a shaft rotation of 360°.
  • the fuel pump 18 and the drive unit 14 are activated accordingly at the moment of the engine cycle which is correct for the cylinder.
  • the engine has several cylinders which are all equipped in the above manner, and the computer 16 may control the normal operation of single or all cylinders.
  • the oil inflow and outflow for the hydraulic drives of the cylinder members are controlled by a spool valve 22, which during normal engine operation is set by an electrically activated positioning means 23 reacting on control signals from the computer 16.
  • the housing 24 of the spool valve is manufactured from several pieces bolted together, viz. a central piece 25 and an end cover 26 on which the electrically activated positioning means 23 is mounted, and an end cover 27 comprising a piston 28 which may be activated by a camshaft, if the electronic control of the engine fails.
  • the central piece of the housing has a fluid inlet conduit 29 communicating with the high-pressure line, which may supply hydraulic oil at a pressure of 300 bar, for example.
  • the central piece of the housing further has two fluid drain conduits 30 communicating with a low-pressure port, and two outlet conduits 31 leading to a pressure chamber 32 in a hydraulic cylinder 33 for the hydraulic drive driving the cylinder member.
  • a hydraulic piston 34 in the drive is driven upwards by the oil pressure in the chamber 32 when the latter is connected with the inlet conduit 29.
  • the piston 34 may be returned to the starting position by means of hydraulic or pneumatic pressure on a piston face, not shown.
  • the conduit 29 opens out in a circumferential groove 35 which is consequently pressurized.
  • the drain conduits 30 communicate with a respective circumferential groove 36
  • the outlet conduits 31 communicate with a respective circumferential groove 37.
  • a spool 38 positioned centrally in the housing is shown in its neutral position where a circumferential flange 39 on the spool exactly bars the groove 37 and thus cuts off the outlet conduit 31 topmost on the drawing from both the drain conduit 30 and the inlet conduit 29.
  • the bottom outlet conduit 31 is cut off from the inlet conduit 29 by means of another circumferential flange 40 on the spool and is cut off from the drain conduit 30 by means of a third circumferential flange 41 on the spool.
  • Two piston members 42 abut on the end cover 27 and project into a respective axially extending bore 43 in the second end of the spool positioned at the end cover 27.
  • bores 43 communicate continuously with the inlet conduit 29.
  • Two piston members 45 at the opposite first end of the spool abuts the end cover 26 and projects into axially extending bores 46.
  • the piston members 45 and the associated bores 46 have a substantially larger diameter than the piston members 42 and their associated bores 43, for example so that the ratio between the areas of the bores is 2:1.
  • Fig. 3 shows that a transverse conduit 47 from each bore 46 opens out into a central longitudinal bore 48 in the spool.
  • the bore 48 is through-going in the full length of the spool, and a small pilot spool 49 is inserted in the bore.
  • Two circumferential grooves 50 and 51 have been so incorporated in the peripheral surface of the pilot spool that a flange 53 positioned centrally between the grooves has a width exactly corresponding to the width of the transverse conduits 47.
  • the groove 50 communicates continuously with the inlet conduit 29 through a pressure conduit 54.
  • Through a drain conduit 55 the groove 51 communicates continuously with the drain conduit 30.
  • the pilot spool is in its neutral position, where the central flange 53 cuts off the transverse conduits 47 from connection with both the pressure conduit 29 and the drain conduit 30.
  • the electrically controlled positioning means 23 is designed according to the linear motor principle, where a movable part 56 carries several windings 57 connected with two U-shaped and therefore freely bendable wires 58, which are so flexible that they cannot prevent, delay or limit the setting movements of the movable part 56 in the longitudinal direction of the spool.
  • the movable part 56 consists of an upper part positioned at right angles to the longitudinal direction of the spool and carrying an annular part projecting to one side, upon which the windings have been fastened, so that the planes of the individual windings are at substantially right angles to the longitudinal axis of the spool.
  • other winding shapes may be used, but that would not give such a good effect of the current applied.
  • a control pin 59 projects through a hole in the movable part 56 and prevents the latter from rotating about the longitudinal axis of the spool.
  • the annular section with the windings of the movable part protrudes down into an oblong slit 60, which is delimited outwards by a strong, annular magnet 61 and inwards by a cylinder-shaped iron-based core material 62.
  • the narrow width of the oblong slit together with the strong magnet contributes to creating a strong magnetic field in the slit.
  • the extent of the slit in the longitudinal direction of the spool is somewhat longer than the maximum setting length of the spool, but for the sake of safety, a soft rubber ring has been disposed at the bottom of the slit to damp the impact of the movable part against the bottom of the slit, in case the member is not stopped by the computer in time.
  • a corresponding damping member 64 is found at the opposite limit stop for the movable part.
  • the movable part is fixed on a connecting rod 65 to which the pilot spool is also fastened. On the side of the movable part 56 turning away from the pilot spool, the rod 65 continues into a position sensor 66 which supplies a continuous position signal to the computer via wires (not shown).
  • the computer continuously determines the intended position of the movable part 56 and thus of the pilot spool and of the spool, which, as explained below, sets itself all the time in the same position as the pilot spool. If the actual position measured by the sensor 66 differs from the intended position, the computer activates a current circuit supplying a current through the windings 57, where the direction and intensity of the current are adapted according to the difference between the actual and the intended positions.
  • the current through the windings causes an electromagnetic force acting on the movable part for displacement in the longitudinal direction of the spool. When there is no current in the windings, the movable part is not affected by a position-changing resultant electromagnetic force.
  • the computer continuously sets the movable part in the intended position.
  • the setting speed may be increased by the computer passing the current one way through the windings during the first half of the position change, and passing an equally large oppositely directed current through the windings during the second half of the position change, whereby the movable part is stopped in exactly the intended position.
  • the setting speed may then be controlled by means of the current intensity.
  • the setting of the spool takes place in the following manner. As mentioned, there is a continuous pressure in the bore 43, which yields a permanent force on the spool directed towards the end cover 26.
  • the spool will always rapidly set itself in the position where the central flange 53 bars the transverse conduits 47.
  • the bores 46 have a larger diameter than the bores 43, there will always be a resulting force on the spool, if it does not occupy the above mentioned neutral position in relation to the pilot spool.
  • the pilot spool is displaced in the longitudinal direction of the spool by influences from the rod 65, the spool will immediately participate in this movement for the above reasons.
  • the small mass of the pilot spool and the associated rod causes the setting forces on the spool to be extremely small, and makes the spool act very rapidly.
  • the piston 28 may be brought into connection with the pilot spool, if a failure of the electronic control occurs.
  • the piston 28 may be omitted and the rod 67 be designed so that it extends down to a cam on a camshaft positioned in alignment with the end cover 27.
  • the spool housing 24 may be designed with only one or with more than two outlet conduits 31 depending on the desired oil flow to the pressure chamber 32.
  • the number of the other connections 29, 30 of the housing and the number of associated circumferential grooves in the housing and flanges on the spool are adapted to the number of outlet conduits.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Magnetically Actuated Valves (AREA)
  • Valve Device For Special Equipments (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Multiple-Way Valves (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Description

The invention relates to a large two-stroke internal combustion engine, such as a main engine of a ship, having at least one hydraulically driven cylinder member, particularly a fuel pump, in which the hydraulic drive of the member comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with a spool valve, the spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the spool is positionable by means of a positioning means electrically activated by a control unit which determines how the cylinder member is to be activated during an engine cycle and from this determines intended positions for the spool, and in which the positioning means includes a linear drive with a movable part which is displaceable in the longitudinal direction of the spool over a distance corresponding to the distance between the extreme positions of the spool.
An engine with such a spool valve is known from W089/03939 but there the movable part is axially positionally locked to the spool, and the positioning means has to move the whole mass of the spool. The linear drive with the movable part is made as a hydraulic cylinder in which the movable piston is axially fixed to the spool. This movable member can influence the spool with very large axially directed forces, but is slow-acting.
For some years it has been usual for the exhaust valve of large two-stroke internal combustion engines to be activated by a hydraulic drive, the driving piston of which is driven by a camshaft. More recently it has been suggested to replace the camshaft activation of the exhaust valve and/or the fuel pump by a hydraulic drive, the driving piston of which is connected with the piston of the fuel pump or delivers oil to the driving piston of the exhaust valve or is directly connected with the spindle of the exhaust valve.
EP-A 0 570 646 was published in November 1993, after the priority date of the present invention. The document describes an internal combustion engine having a hydraulically driven fuel pump, in which the hydraulic drive comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with a spool valve, the first spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the first spool is positionable by means of a positioning means electrically activated to control the fuel pump, and in which the positioning means includes a linear drive with a movable part which is displaceable in the longitudinal direction of the spool, and in which the movable part carries windings positioned in a magnetic field, and in which the movable part is connected with a second spool that is axially displaceable, and in which a sensor detects the position of the first spool. The first spool is moved proportionally to the movements of the second spool, the second spool can only be moved short distances, it has a relatively large mass, it is positionally suspended between mechanical springs, and there is no position feed-back to a control unit.
In internal combustion engines with hydraulic drives it is desirable to obtain an accurate control of hydraulic systems, and a very well-defined, rapid and accurate control of the pressure on the delivery side of the hydraulic drive. It is known to use pressure relief valves on the high-pressure side of the drive, but these known hydraulic systems are often quite complicated in order to obtain a sufficiently accurate control of pressure conditions in the systems.
The object of the invention is to provide a large two-stroke internal combustion engine with a hydraulic drive which is quick-acting and may be set accurately, and at the same time is of a simple design.
This is obtained by the engine according to the invention being characterized in that the movable part carries windings positioned in a magnetic field in a slit which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings, that the movable part is connected with a small pilot spool which is axially displaceable with respect to the spool, that a sensor signals the actual position of the movable part to the control unit, that the spool follows the movements of the pilot spool, and that the control unit supplies current to the windings, if the actual position of the movable part differs from the intended position.
With a linear motor where the mass of the movable part is reduced owing to the part only having to carry the windings, it is possible to obtain very rapid and accurate setting movements, which may extend over any length. Thus, in a simple manner it is possible to let the movable part be displaceable over the same distance as the spool, whereby the design of the spool valve becomes very simple. The possibility provided with such a spool valve for an accurate and extremely rapid control of the oil pressure on the delivery side of the hydraulic drive is particularly advantageous in a diesel engine, where particularly the movements of the fuel pump have to be controlled very accurately to obtain an optimum combustion process in the combustion chamber of the engine. The hydraulic drive for the fuel pump can control initiation and termination of the fuel injection at exactly the desired moment of the engine cycle and with delivery of an accurately metered amount of oil. The accurate control of the fuel injection renders it possible to reduce the specific fuel oil consumption of the engine, and further, the fuel injection may be divided into a pre-injection and a main injection merely by starting and stopping the hydraulic drive several times during a relatively small angle of rotation of the crankshaft.
With the positioning means designed as a linear motor, the mass of the positioning means has been made so small that the setting speed is substantially determined by the mass to be moved by the positioning means. This makes it possible to obtain novel high setting speeds for the spool valve by limiting the mass connected to the movable part. For a spool with a mass of approximately 1 kg, the pilot spool may, for example, be designed with a mass of 10 g, which, for example, makes possible a spool move of 15 mm in 3-4 ms. This by far exceeds the setting speed obtainable so far for relatively large spool valves controlling high-pressure hydraulic drives. The possibility of rapidly opening the spool valve for supply of large amounts of oil, and corresponding rapid resetting of the spool valve for relief of the pressure in the hydraulic cylinder renders possible a very fine control of the pressure on the delivery side of the hydraulic drive.
By means of the positioning sensor, the control unit may continuously monitor whether the spool is in the desired position. If the spool changes position owing to external influences, the control unit may immediately pass a corrective flash of current through the windings so that the actual position is made to correspond with the intended position.
It is essential for obtaining the rapid movements of the spool, and thus its short setting times intended with the invention, that the windings are positioned on the movable part so that the latter achieves a very low mass.
The current intensity required for the position setting depends on the strength of the magnetic field in the oblong slit. Preferably, therefore, the side walls of the slit are delimited by an annular magnet and an iron-based material, respectively, as this in a simple manner produces a strong and uniform magnetic field which renders it possible to limit the size of the windings, in order that the already small mass of the movable part is reduced as much as possible, which promotes a rapid setting of the spool valve.
Preferably, the movable part is in controlling connection with the spool via a rod extending coaxially with the spool and upon which the movable part is rigidly mounted. This makes it possible to arrange the positioning means on the outside of the spool valve housing itself, thus facilitating the manufacturing and maintenance of the valve.
The pilot spool functions by controlling control edges for high-pressure and low-pressure oil sources which may affect pressure faces in the spool.
In an embodiment preferred owing to its fast-acting character, the internal combustion engine is characterized in that at its first end the spool has an axially extending bore which communicates with the high-pressure source, and in which a piston supported by the spool housing is displaceably inserted in a tightly fitting manner, that at its second end the spool has an axially extending bore in which a piston supported by the spool housing is displaceably inserted in a tightly fitting manner, that the bore at the second end of the spool has a conduit extending to the pilot spool and having a mouth which may be barred by the flange of the pilot spool, and that the bore at the second end of the spool has a larger cross sectional area than the bore at the first end of the spool.
The high-pressure connection to the smallest bore at the first end of the spool causes a permanent force on the spool acting in a direction towards the second end of the spool. If this force displaces the spool in relation to the pilot spool, the conduit mouth is opened at the pilot spool flange to the high-pressure source, so that the pressure in the large bore at the second end of the spool is increased, whereby a force directed towards the first end of the spool increases, so that the spool again occupies a neutral position in relation to the pilot spool, in which position the two oppositely directed forces balance. If the pressure in the large bore becomes too high, the spool is displaced so that the conduit mouth is brought into contact with the low-pressure port, thus relieving the pressure in the large bore to the level of balance. As the bore at the second end of the spool has the largest cross sectional area, a displacement of the pilot spool will always cause a corresponding displacement of the spool. The setting speed of the spool in relation to the pilot spool may be freely selected by adapting the mutual cross sectional area between the large and the small bore at either end of the spool. Of course, it is possible to design several axially extending bores with associated pistons at each spool end, when care is taken to give the bores a different total cross sectional area.
The pilot spool can be positioned inside the spool, preferably coaxially with it, and may have two circumferential grooves in its peripheral surface and a flange positioned between the grooves, which two grooves of the pilot spool communicate with the high-pressure source and the low-pressure port, respectively.
The use of a small pilot spool makes it simple to provide a camshaft-activated emergency control which enters into force in case of failure in the electronic system of the engine, as the spool is in that case activated via a rod following the movements of a control cam rotating synchronously with the crankshaft of the engine. The rod may be directly activated by the cam, but it is also possible to use an indirect, hydraulically based emergency control system, as described in W094/29577.
The present invention also relates to a spool valve for control of a hydraulic drive, such as a drive for a fuel pump or an exhaust valve of an internal combustion engine, in which the hydraulic drive comprises a driving piston journalled in a hydraulic cylinder which, through a flow passage, is in communication with the spool valve, the spool of which may occupy a position in which the flow passage is connected with a high pressure source for hydraulic oil, and another position, where the flow passage is connected with a low pressure port, and in which the spool is positionable by means of a positioning means electrically activated by a control unit, and in which the positioning means has a movable part and a sensor signalizing the actual position of the movable part to the control unit which determines intended positions for the spool and for a movable part. This spool valve is characterized in that the movable part carries windings positioned in a magnetic field in a slit which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings, that the movable part is connected with a small pilot spool which is axially displaceable with respect to the spool, that the spool follows the movements of the pilot spool, that the control unit supplies current to the windings, if the actual position of the movable part differs from the intended position, that at its first end the spool has an axially extending bore which communicates with the high-pressure source, and in which a piston supported by the spool housing is displaceably inserted, that at its second end the spool has an axially extending bore in which a piston supported by the spool housing is displaceably inserted, that the bore at the second end of the spool has a conduit extending to the pilot spool and having a mouth which may be barred by a flange of the pilot spool, and that the bore at the second end of the spool has a larger cross sectional area than the bore at the first end of the spool.
As mentioned above, the positioning means is designed as a linear motor with movable windings and with positioning feedback to the control unit. By letting the spool follow the movements of the movable part with the pilot spool, an unambiguous and well-defined coherence between the control of the positioning means and the control of the hydraulic drive is obtained in a simple manner. From the driving unit of a loudspeaker it is known to use a movable part with windings positioned in a magnetic field in an oblong slit. In the loudspeaker, the windings are fed with an alternating voltage of a frequency which causes a corresponding oscillation frequency in the membrane connected with the movable part. As these oscillation frequencies may get above 20,000 Hz, it is obvious that the movable part may perform even extremely rapid setting movements. By supplying direct current to such a winding-carrying part, the control unit may cause very rapid movements in the part and the associated spool. The maximum travel of the movable part may be freely selected according to need by designing the oblong slit with a larger length than the largest travel desired from the movable part. The movable part only moves when current passes through the windings, and the desired direction, magnitude and speed of the movement may be freely selected by adaptation of the current intensity and the current direction of the windings. The movable part may thus rapidly be started and stopped immediately at any desired intermediate position between the extreme positions.
Examples of embodiments of the invention will be described below in further detail with reference to the schematic drawings, in which
  • Fig. 1 is an outline of an internal combustion engine,
  • Fig. 2 is a longitudinal sectional view through a spool valve for a cylinder member,
  • Fig. 3, on a larger scale, is a segment of the spool valve of Fig. 2,
  • Fig. 4, on a larger scale, shows a positioning means for the spool valve of Fig. 2.
  • Fig. 1 shows a large two-stroke diesel engine of the crosshead type generally designated 1, which may be used as the main engine of a ship or as a stationary power-producing engine. The combustion chamber 2 of the engine is delimited by a cylinder liner 3 and a cylinder cover 4 and a piston 5 journalled in the liner.
    Via a piston rod 6, the piston is directly connected with a crosshead 7 which, via a connecting rod 8, is directly connected with a connecting rod pin 9 in a throw 10 of a crankshaft 11. A cylinder member in the form of an exhaust valve 12 with associated housing 13 is mounted on the cover 4. The exhaust valve is activated by a hydraulic drive 14 controlled by an electro-mechanical spool valve activated by control signals transmitted through a wire 15 from a computer 16.
    A fuel valve 17 mounted in the cover 4 may supply atomized fuel to the combustion chamber 2. Another cylinder member in the form of a fuel pump 18 is controlled by an electro-mechanical spool valve and may supply fuel to the fuel valve through a pressure line 19 in dependency of control signals received from the computer 16 through a wire 20. Through a signal-transmitting wire 21 the computer 16 is supplied with information on the actual number of revolutions per minute of the engine. The number of revolutions may either be taken from the tachometer of the engine, or it may originate from an angle detector and indicator mounted on the main shaft of the engine and determining the actual angular position and rotating speed of the engine for intervals constituting fractions of an engine cycle of a shaft rotation of 360°. When the computer has determined the time for the fuel injection and the associated amount of fuel, and the opening and closing times of the exhaust valve, the fuel pump 18 and the drive unit 14 are activated accordingly at the moment of the engine cycle which is correct for the cylinder. The engine has several cylinders which are all equipped in the above manner, and the computer 16 may control the normal operation of single or all cylinders.
    The oil inflow and outflow for the hydraulic drives of the cylinder members are controlled by a spool valve 22, which during normal engine operation is set by an electrically activated positioning means 23 reacting on control signals from the computer 16.
    The housing 24 of the spool valve is manufactured from several pieces bolted together, viz. a central piece 25 and an end cover 26 on which the electrically activated positioning means 23 is mounted, and an end cover 27 comprising a piston 28 which may be activated by a camshaft, if the electronic control of the engine fails.
    The central piece of the housing has a fluid inlet conduit 29 communicating with the high-pressure line, which may supply hydraulic oil at a pressure of 300 bar, for example. The central piece of the housing further has two fluid drain conduits 30 communicating with a low-pressure port, and two outlet conduits 31 leading to a pressure chamber 32 in a hydraulic cylinder 33 for the hydraulic drive driving the cylinder member. A hydraulic piston 34 in the drive is driven upwards by the oil pressure in the chamber 32 when the latter is connected with the inlet conduit 29. When the chamber 32 is connected with the drain conduit 30, the piston 34 may be returned to the starting position by means of hydraulic or pneumatic pressure on a piston face, not shown.
    The conduit 29 opens out in a circumferential groove 35 which is consequently pressurized. Similarly, the drain conduits 30 communicate with a respective circumferential groove 36, and the outlet conduits 31 communicate with a respective circumferential groove 37. A spool 38 positioned centrally in the housing is shown in its neutral position where a circumferential flange 39 on the spool exactly bars the groove 37 and thus cuts off the outlet conduit 31 topmost on the drawing from both the drain conduit 30 and the inlet conduit 29. Similarly, the bottom outlet conduit 31 is cut off from the inlet conduit 29 by means of another circumferential flange 40 on the spool and is cut off from the drain conduit 30 by means of a third circumferential flange 41 on the spool.
    When the spool is moved from its neutral position towards the positioning means 23, the inlet conduit 29 is put into connection with the two outlet conduits 31, and when the spool is moved from its starting position towards the end cover 27, the drain conduits 30 are put into connection with the two outlet conduits 31.
    Two piston members 42, of which only one is shown in the drawing, abut on the end cover 27 and project into a respective axially extending bore 43 in the second end of the spool positioned at the end cover 27. Through a pressure conduit 44, bores 43 communicate continuously with the inlet conduit 29. Two piston members 45 at the opposite first end of the spool abuts the end cover 26 and projects into axially extending bores 46. The piston members 45 and the associated bores 46 have a substantially larger diameter than the piston members 42 and their associated bores 43, for example so that the ratio between the areas of the bores is 2:1.
    Fig. 3 shows that a transverse conduit 47 from each bore 46 opens out into a central longitudinal bore 48 in the spool. The bore 48 is through-going in the full length of the spool, and a small pilot spool 49 is inserted in the bore. Two circumferential grooves 50 and 51 have been so incorporated in the peripheral surface of the pilot spool that a flange 53 positioned centrally between the grooves has a width exactly corresponding to the width of the transverse conduits 47. The groove 50 communicates continuously with the inlet conduit 29 through a pressure conduit 54. Through a drain conduit 55, the groove 51 communicates continuously with the drain conduit 30. In the position shown, the pilot spool is in its neutral position, where the central flange 53 cuts off the transverse conduits 47 from connection with both the pressure conduit 29 and the drain conduit 30.
    The electrically controlled positioning means 23 is designed according to the linear motor principle, where a movable part 56 carries several windings 57 connected with two U-shaped and therefore freely bendable wires 58, which are so flexible that they cannot prevent, delay or limit the setting movements of the movable part 56 in the longitudinal direction of the spool. The movable part 56 consists of an upper part positioned at right angles to the longitudinal direction of the spool and carrying an annular part projecting to one side, upon which the windings have been fastened, so that the planes of the individual windings are at substantially right angles to the longitudinal axis of the spool. Of course, other winding shapes may be used, but that would not give such a good effect of the current applied.
    A control pin 59 projects through a hole in the movable part 56 and prevents the latter from rotating about the longitudinal axis of the spool. The annular section with the windings of the movable part protrudes down into an oblong slit 60, which is delimited outwards by a strong, annular magnet 61 and inwards by a cylinder-shaped iron-based core material 62. The narrow width of the oblong slit together with the strong magnet contributes to creating a strong magnetic field in the slit. The extent of the slit in the longitudinal direction of the spool is somewhat longer than the maximum setting length of the spool, but for the sake of safety, a soft rubber ring has been disposed at the bottom of the slit to damp the impact of the movable part against the bottom of the slit, in case the member is not stopped by the computer in time. A corresponding damping member 64 is found at the opposite limit stop for the movable part. The movable part is fixed on a connecting rod 65 to which the pilot spool is also fastened. On the side of the movable part 56 turning away from the pilot spool, the rod 65 continues into a position sensor 66 which supplies a continuous position signal to the computer via wires (not shown).
    The computer continuously determines the intended position of the movable part 56 and thus of the pilot spool and of the spool, which, as explained below, sets itself all the time in the same position as the pilot spool. If the actual position measured by the sensor 66 differs from the intended position, the computer activates a current circuit supplying a current through the windings 57, where the direction and intensity of the current are adapted according to the difference between the actual and the intended positions. The current through the windings causes an electromagnetic force acting on the movable part for displacement in the longitudinal direction of the spool. When there is no current in the windings, the movable part is not affected by a position-changing resultant electromagnetic force.
    Now, the functioning of the spool valve will be described. The computer continuously sets the movable part in the intended position. When the intended position has to be changed, the setting speed may be increased by the computer passing the current one way through the windings during the first half of the position change, and passing an equally large oppositely directed current through the windings during the second half of the position change, whereby the movable part is stopped in exactly the intended position. The setting speed may then be controlled by means of the current intensity. The setting of the spool takes place in the following manner. As mentioned, there is a continuous pressure in the bore 43, which yields a permanent force on the spool directed towards the end cover 26. When the pilot spool stands still, it is possible that this force will displace the spool in the direction of the cover 26. If this happens, the transverse conduits 47 are put into communication with the pressure conduit 54, so that pressurized oil flows into the bores 46. The consequent pressure increase in the chamber in front of the piston members 45 acts on the spool with a force which is directed towards the cover 27 and forces the spool to occupy the position in which the central flange 53 of the pilot spool exactly bars the transverse conduits 47. If the pressure in the bores 46 becomes too great, the spool is moved a fraction towards the cover 26, thus putting the transverse conduits 47 into communication with the drain conduit 55, so that the overpressure in the bores 46 is relieved to the level of balance, where the oppositely directed forces on the spool have the same magnitude.
    It is seen from this that the spool will always rapidly set itself in the position where the central flange 53 bars the transverse conduits 47. As the bores 46 have a larger diameter than the bores 43, there will always be a resulting force on the spool, if it does not occupy the above mentioned neutral position in relation to the pilot spool. When the pilot spool is displaced in the longitudinal direction of the spool by influences from the rod 65, the spool will immediately participate in this movement for the above reasons. The small mass of the pilot spool and the associated rod causes the setting forces on the spool to be extremely small, and makes the spool act very rapidly.
    Through a rod 67, the piston 28 may be brought into connection with the pilot spool, if a failure of the electronic control occurs. Instead of a hydraulic transfer of the cam movement to the piston 28, the piston 28 may be omitted and the rod 67 be designed so that it extends down to a cam on a camshaft positioned in alignment with the end cover 27.
    The spool housing 24 may be designed with only one or with more than two outlet conduits 31 depending on the desired oil flow to the pressure chamber 32. The number of the other connections 29, 30 of the housing and the number of associated circumferential grooves in the housing and flanges on the spool are adapted to the number of outlet conduits.

    Claims (9)

    1. A large two-stroke internal combustion engine, such as a main engine of a ship, having at least one hydraulically driven cylinder member, particularly a fuel pump (18), in which the hydraulic drive of the member comprises a driving piston (34) journalled in a hydraulic cylinder (33) which, through a flow passage (31), is in communication with a spool valve, the spool (38) of which may occupy a position in which the flow passage is connected with a high pressure source (29) for hydraulic oil, and another position, where the flow passage is connected with a low pressure port (30), and in which the spool is positionable by means of a positioning means (23) electrically activated by a control unit (16) which determines how the cylinder member is to be activated during an engine cycle and from this determines intended positions for the spool, and in which the positioning means includes a linear drive with a movable part (56) which is displaceable in the longitudinal direction of the spool over a distance corresponding to the distance between the extreme positions of the spool, characterized in that the movable part carries windings (57) positioned in a magnetic field in a slit (60) which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings (57), that the movable part is connected with a small pilot spool (49) which is axially displaceable with respect to the spool, that a sensor (66) signals the actual position of the movable part to the control unit, that the spool (38) follows the movements of the pilot spool, and that the control unit (16) supplies current to the windings, if the actual position of the movable part differs from the intended position.
    2. An internal combustion engine according to claim 1, characterized in that the side walls of the slit (60) are delimited by an annular magnet (61) and an iron-based material (62), respectively.
    3. An internal combustion engine according to claim 1 or 2, characterized in that the movable part (56) is in controlling connection with the spool (38) via a rod (65) extending coaxially with the spool and upon which the movable part and the pilot spool are mounted.
    4. An internal combustion engine according to any one of claims 1-3, characterized in that that at its first end the spool has an axially extending bore (43) which communicates with the high-pressure source, and in which a piston (42) supported by the spool housing is displaceably inserted, that at its second end the spool has an axially extending bore (46) in which a piston (45) supported by the spool housing is displaceably inserted, that the bore at the second end of the spool has a conduit (47) extending to the pilot spool and having a mouth which may be barred by a flange of the pilot spool, and that the bore (46) at the second end of the spool has a larger cross sectional area than the bore (43) at the first end of the spool.
    5. An internal combustion engine according to claim 4, characterized in that the pilot spool (49) is positioned inside the spool, preferably coaxially with it, and has two circumferential grooves (50, 51) in its peripheral surface, that the flange (53) is positioned between the grooves, and that the two grooves of the pilot spool communicate with the high-pressure source (29) and the low-pressure port (30), respectively.
    6. An internal combustion engine according to any one of claims 1-5, characterized in that in case of failure in the electronic control system of the engine, the pilot spool may be activated via a rod (67) following the movements of a control cam rotating synchronously with the crankshaft of the engine.
    7. A spool valve (22) for control of a hydraulic drive, such as a drive for a fuel pump (18) or an exhaust valve (12) of an internal combustion engine, in which the hydraulic drive comprises a driving piston (34) journalled in a hydraulic cylinder (33) which, through a flow passage (31), is in communication with the spool valve, the spool (38) of which may occupy a position in which the flow passage is connected with a high pressure source (29) for hydraulic oil, and another position, where the flow passage is connected with a low pressure port (30), and in which the spool is positionable by means of a positioning means (23) electrically activated by a control unit (16), and in which the positioning means has a movable part and a sensor (66) signalizing the actual position of the movable part to the control unit which determines intended positions for the spool and for a movable part (56), characterized in that the movable part carries windings (57) positioned in a magnetic field in a slit (60) which is oblong in the longitudinal direction of the spool, that the movable part is displaceable in the longitudinal direction of the slit in dependency of the direction and intensity of the current in the windings (57), that the movable part is connected with a small pilot spool (49) which is axially displaceable with respect to the spool, that the spool (38) follows the movements of the pilot spool, that the control unit (16) supplies current to the windings, if the actual position of the movable part differs from the intended position, that at its first end the spool has an axially extending bore (43) which communicates with the high-pressure source, and in which a piston (42) supported by the spool housing is displaceably inserted, that at its second end the spool has an axially extending bore (46) in which a piston (45) supported by the spool housing is displaceably inserted, that the bore at the second end of the spool has a conduit (47) extending to the pilot spool and having a mouth which may be barred by a flange of the pilot spool, and that the bore (46) at the second end of the spool has a larger cross sectional area than the bore (43) at the first end of the spool.
    8. A spool valve according to claim 7, characterized in that the pilot spool (49) is positioned inside the spool, preferably coaxially with it, and has two circumferential grooves (50, 51) in its peripheral surface, that the flange (53) is positioned between the grooves, and that the two grooves of the pilot spool communicate with the high-pressure source (29) and the low-pressure port (30), respectively.
    9. A spool valve according to claim 7 or 8, characterized in that the movable part (56) is in controlling connection with the spool (38) via a rod (65) extending coaxially with the spool and upon which the movable part and the pilot spool are mounted.
    EP94902643A 1993-06-04 1993-12-02 Large two-stroke internal combustion engine with slide valve Expired - Lifetime EP0701653B1 (en)

    Applications Claiming Priority (4)

    Application Number Priority Date Filing Date Title
    DK646/93 1993-06-04
    DK064693A DK170121B1 (en) 1993-06-04 1993-06-04 Sliding valve and large two stroke internal combustion engine
    DK64693 1993-06-04
    PCT/DK1993/000400 WO1994029578A1 (en) 1993-06-04 1993-12-02 A slide valve and a large two-stroke internal combustion engine

    Publications (2)

    Publication Number Publication Date
    EP0701653A1 EP0701653A1 (en) 1996-03-20
    EP0701653B1 true EP0701653B1 (en) 1998-07-29

    Family

    ID=8095952

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP94902643A Expired - Lifetime EP0701653B1 (en) 1993-06-04 1993-12-02 Large two-stroke internal combustion engine with slide valve

    Country Status (11)

    Country Link
    US (1) US5732678A (en)
    EP (1) EP0701653B1 (en)
    JP (1) JP3164822B2 (en)
    KR (1) KR100310083B1 (en)
    CN (1) CN1105098A (en)
    AU (1) AU5693794A (en)
    DE (1) DE69320068T2 (en)
    DK (1) DK170121B1 (en)
    ES (1) ES2116208B1 (en)
    FI (1) FI106880B (en)
    WO (1) WO1994029578A1 (en)

    Families Citing this family (42)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US7281527B1 (en) * 1996-07-17 2007-10-16 Bryant Clyde C Internal combustion engine and working cycle
    US6951211B2 (en) 1996-07-17 2005-10-04 Bryant Clyde C Cold air super-charged internal combustion engine, working cycle and method
    US8215292B2 (en) 1996-07-17 2012-07-10 Bryant Clyde C Internal combustion engine and working cycle
    US7222614B2 (en) 1996-07-17 2007-05-29 Bryant Clyde C Internal combustion engine and working cycle
    DK173815B1 (en) * 1997-05-28 2001-11-12 Man B & W Diesel As Hydraulically activated fuel pump for an internal combustion engine
    US5865156A (en) * 1997-12-03 1999-02-02 Caterpillar Inc. Actuator which uses fluctuating pressure from an oil pump that powers a hydraulically actuated fuel injector
    US6604497B2 (en) * 1998-06-05 2003-08-12 Buehrle, Ii Harry W. Internal combustion engine valve operating mechanism
    US6044815A (en) * 1998-09-09 2000-04-04 Navistar International Transportation Corp. Hydraulically-assisted engine valve actuator
    US6349686B1 (en) * 2000-08-31 2002-02-26 Caterpillar Inc. Hydraulically-driven valve and hydraulic system using same
    US7178492B2 (en) 2002-05-14 2007-02-20 Caterpillar Inc Air and fuel supply system for combustion engine
    US6688280B2 (en) * 2002-05-14 2004-02-10 Caterpillar Inc Air and fuel supply system for combustion engine
    US7201121B2 (en) 2002-02-04 2007-04-10 Caterpillar Inc Combustion engine including fluidically-driven engine valve actuator
    US20050247286A1 (en) * 2002-02-04 2005-11-10 Weber James R Combustion engine including fluidically-controlled engine valve actuator
    US6732685B2 (en) * 2002-02-04 2004-05-11 Caterpillar Inc Engine valve actuator
    US7347171B2 (en) * 2002-02-04 2008-03-25 Caterpillar Inc. Engine valve actuator providing Miller cycle benefits
    US7069887B2 (en) 2002-05-14 2006-07-04 Caterpillar Inc. Engine valve actuation system
    US7004122B2 (en) * 2002-05-14 2006-02-28 Caterpillar Inc Engine valve actuation system
    US20050241597A1 (en) * 2002-05-14 2005-11-03 Weber James R Air and fuel supply system for a combustion engine
    US20050247284A1 (en) * 2002-05-14 2005-11-10 Weber James R Air and fuel supply system for combustion engine operating at optimum engine speed
    US20050235950A1 (en) * 2002-05-14 2005-10-27 Weber James R Air and fuel supply system for combustion engine
    US6941909B2 (en) * 2003-06-10 2005-09-13 Caterpillar Inc System and method for actuating an engine valve
    US7252054B2 (en) 2002-05-14 2007-08-07 Caterpillar Inc Combustion engine including cam phase-shifting
    US7191743B2 (en) * 2002-05-14 2007-03-20 Caterpillar Inc Air and fuel supply system for a combustion engine
    DE10311493B4 (en) 2003-03-15 2005-01-05 Man B & W Diesel A/S Two-stroke diesel engine
    DE10325067B3 (en) 2003-06-03 2005-01-13 Man B & W Diesel A/S Control apparatus for two-stroke large sized engine, has servo-valve slider which can be slid into main-valve slider to control at least one of flow paths arranged in main-valve slider
    US6912458B2 (en) * 2003-06-25 2005-06-28 Caterpillar Inc Variable valve actuation control for operation at altitude
    CN100354558C (en) * 2003-07-09 2007-12-12 株式会社纳博克 Slide valve for ship use
    WO2005019619A1 (en) * 2003-08-18 2005-03-03 Bryant, Clyde, C. Improved internal combustion engine and working cycle
    DE10361221B4 (en) 2003-12-24 2006-03-09 Man B&W Diesel A/S Device for controlling the time-shifted connection of two acted upon by a pressure medium units with a pressure medium source
    JP2006029247A (en) * 2004-07-20 2006-02-02 Denso Corp Engine stop / start control device
    JP2008527239A (en) * 2005-02-02 2008-07-24 エムエーエヌ・ディーゼル・エーエス Large 2-cycle diesel engine with hydraulically operated exhaust gas valve
    US7201096B2 (en) * 2005-06-06 2007-04-10 Caterpillar Inc Linear motor having a magnetically biased neutral position
    JP4592770B2 (en) * 2008-02-27 2010-12-08 エムエーエヌ・ディーゼル・アンド・ターボ・フィリアル・アフ・エムエーエヌ・ディーゼル・アンド・ターボ・エスイー・ティスクランド Variable valve timing for large two-stroke diesel engines with camshafts
    DK177283B1 (en) 2010-02-24 2012-10-08 Man Diesel & Turbo Deutschland Valve arrangement
    DK177410B1 (en) 2010-02-24 2013-04-02 Man Diesel & Turbo Deutschland Valve actuation system for a large two stroke diesel engine
    DE102010023698A1 (en) * 2010-06-14 2011-12-15 Continental Automotive Gmbh Injector with direct and servo drive
    US9909678B2 (en) * 2010-08-10 2018-03-06 Ross Europa Gmbh Two part valve
    US8453619B2 (en) * 2011-01-04 2013-06-04 GM Global Technology Operations LLC Hydraulic engine valve actuation system including independent feedback control
    DK177695B1 (en) * 2012-11-16 2014-03-17 Man Diesel & Turbo Deutschland A large slow running turbocharged two-stoke uniflow internal combustion engine with crosshead and a cam driven exhaust valve actuation system
    US9494246B1 (en) 2014-07-22 2016-11-15 Google Inc. Linear hydraulic valve
    US10920905B2 (en) * 2019-03-19 2021-02-16 Trek Bicycle Corporation Universal fatigue valve system
    CN114961916B (en) * 2021-11-24 2024-06-14 中国船舶集团有限公司第七一一研究所 Mechanical hydraulic control device and variable valve mechanism

    Citations (7)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE3208651A1 (en) * 1981-03-23 1982-10-07 Hitachi, Ltd., Tokyo SERVO VALVE DEVICE
    DE3345880A1 (en) * 1982-12-20 1984-06-20 Hitachi, Ltd., Tokio/Tokyo DIRECT ACTING CONTROL VALVE
    GB2136499A (en) * 1983-03-15 1984-09-19 Solex Supplying gaseous fuel to internal combustion engines
    GB2138969A (en) * 1983-04-19 1984-10-31 Ishikawajima Harima Heavy Ind Direct drive electro-hydraulic servo valves
    WO1989003939A1 (en) * 1987-10-20 1989-05-05 Nova-Werke Ag Linear drive with hydraulic reinforcement
    US5076537A (en) * 1990-07-19 1991-12-31 Evc, Inc. Electromechanical servovalve
    EP0570649A1 (en) * 1992-05-19 1993-11-24 New Sulzer Diesel Ag Device for controlling a hydraulic fluid flow, especially for fuel injection to an internal combustion engine

    Family Cites Families (15)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US2597443A (en) * 1949-08-06 1952-05-20 Arthur E Broughton Oscillator
    US2953123A (en) * 1959-10-30 1960-09-20 Textron Electronics Inc Electrohydraulic servo valve
    FR2067780A5 (en) * 1969-11-15 1971-08-20 Applic Mach Motrices
    DE2236919A1 (en) * 1972-07-27 1974-02-07 Rexroth Gmbh G L HYDRAULIC SENSOR VALVE
    US4041983A (en) * 1975-07-09 1977-08-16 Caterpillar Tractor Co. Pressure controlled swing valve with safety feature
    JPS6048641B2 (en) * 1976-06-11 1985-10-29 株式会社日立製作所 fluid pressure servo valve
    JPS5316183A (en) * 1976-07-28 1978-02-14 Hitachi Ltd Fluid pressure driving device
    JPS5814954B2 (en) * 1979-07-02 1983-03-23 株式会社日立製作所 Direct-acting servo valve
    JPS5686281A (en) * 1979-12-17 1981-07-13 Hitachi Ltd Oil pressure servo valve
    JPS56143883A (en) * 1980-04-09 1981-11-09 Hitachi Ltd Multistage hydraulic servo-valve
    US4462368A (en) * 1980-07-10 1984-07-31 Diesel Kiki Company, Ltd. Fuel injection system for internal combustion engine
    EP0344122A1 (en) * 1988-05-27 1989-11-29 SIG Schweizerische Industrie-Gesellschaft Multi-edge detection valve
    GB9112957D0 (en) * 1991-06-15 1991-08-07 Carver & Co Eng Flow control valve
    US5248123A (en) * 1991-12-11 1993-09-28 North American Philips Corporation Pilot operated hydraulic valve actuator
    DK170122B1 (en) * 1993-06-04 1995-05-29 Man B & W Diesel Gmbh Large two stroke internal combustion engine

    Patent Citations (7)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE3208651A1 (en) * 1981-03-23 1982-10-07 Hitachi, Ltd., Tokyo SERVO VALVE DEVICE
    DE3345880A1 (en) * 1982-12-20 1984-06-20 Hitachi, Ltd., Tokio/Tokyo DIRECT ACTING CONTROL VALVE
    GB2136499A (en) * 1983-03-15 1984-09-19 Solex Supplying gaseous fuel to internal combustion engines
    GB2138969A (en) * 1983-04-19 1984-10-31 Ishikawajima Harima Heavy Ind Direct drive electro-hydraulic servo valves
    WO1989003939A1 (en) * 1987-10-20 1989-05-05 Nova-Werke Ag Linear drive with hydraulic reinforcement
    US5076537A (en) * 1990-07-19 1991-12-31 Evc, Inc. Electromechanical servovalve
    EP0570649A1 (en) * 1992-05-19 1993-11-24 New Sulzer Diesel Ag Device for controlling a hydraulic fluid flow, especially for fuel injection to an internal combustion engine

    Non-Patent Citations (1)

    * Cited by examiner, † Cited by third party
    Title
    IBM Technical Disclosure Bulletin, Bd.6,Nr.5,Oct.1963 *

    Also Published As

    Publication number Publication date
    DE69320068D1 (en) 1998-09-03
    AU5693794A (en) 1995-01-03
    ES2116208A1 (en) 1998-07-01
    EP0701653A1 (en) 1996-03-20
    CN1105098A (en) 1995-07-12
    FI955833A7 (en) 1995-12-04
    JPH08511072A (en) 1996-11-19
    KR960702882A (en) 1996-05-23
    FI955833A0 (en) 1995-12-04
    US5732678A (en) 1998-03-31
    DK170121B1 (en) 1995-05-29
    FI106880B (en) 2001-04-30
    DE69320068T2 (en) 1999-04-15
    ES2116208B1 (en) 1999-03-01
    DK64693A (en) 1994-12-05
    WO1994029578A1 (en) 1994-12-22
    JP3164822B2 (en) 2001-05-14
    KR100310083B1 (en) 2002-06-20
    DK64693D0 (en) 1993-06-04

    Similar Documents

    Publication Publication Date Title
    US5732678A (en) Slide valve and a large two-stroke internal combustion engine
    EP0701652B1 (en) A large two-stroke internal combustion engine
    JP3382520B2 (en) Cylinder lubrication device for multi-cylinder internal combustion engine
    CA1229541A (en) Pressure regulator
    CA1072817A (en) Pilot operated pressure compensated pump control
    GB2097858A (en) A fuel injector for an internal combustion engine
    US4498442A (en) Fuel injection pump
    US5329890A (en) Hydraulic control device
    US4241714A (en) Solenoid valve controlled fuel injection pump
    CA2007346A1 (en) Fluid-controlled servo-arrangement
    US5056414A (en) Linear drive with hydraulic amplification
    US4170976A (en) Control device for diesel-injection internal combustion engines
    US5050558A (en) Fuel injection pump for internal-combustion engines
    JPH01200057A (en) Fuel injector for internal combustion engine
    JPH0350379A (en) Fuel injection pump for internal- combustion engine
    US4604980A (en) Fuel injection pump
    JP2001526755A (en) Method of operating hydraulically operated fuel pump for internal combustion engine and hydraulically operated fuel pump
    JP3974614B2 (en) Device for controlling the off-time connection between two pressure medium impact collective machines and one pressure medium source
    US4393846A (en) Fuel pumping apparatus
    GB2196153A (en) Fuel system for a multi-cylinder engine
    JP2000054817A (en) Hydraulic control device for lubrication circuit of internal combustion engine
    US4951459A (en) Methods for metering fluid and apparatus for use therewith
    US4825751A (en) Controlled bypass and flow-control valve unit for hydraulic power steering system
    US6453880B1 (en) Fuel injection pump
    US5580223A (en) Fuel injection pump for internal combustion engines

    Legal Events

    Date Code Title Description
    PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

    Free format text: ORIGINAL CODE: 0009012

    17P Request for examination filed

    Effective date: 19951027

    AK Designated contracting states

    Kind code of ref document: A1

    Designated state(s): DE FR IT

    17Q First examination report despatched

    Effective date: 19970507

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAH Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOS IGRA

    GRAH Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOS IGRA

    GRAA (expected) grant

    Free format text: ORIGINAL CODE: 0009210

    AK Designated contracting states

    Kind code of ref document: B1

    Designated state(s): DE FR IT

    REF Corresponds to:

    Ref document number: 69320068

    Country of ref document: DE

    Date of ref document: 19980903

    ET Fr: translation filed
    PLBE No opposition filed within time limit

    Free format text: ORIGINAL CODE: 0009261

    STAA Information on the status of an ep patent application or granted ep patent

    Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

    26N No opposition filed
    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: FR

    Payment date: 20021206

    Year of fee payment: 10

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: FR

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20040831

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: ST

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: IT

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20051202

    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: DE

    Payment date: 20121220

    Year of fee payment: 20

    REG Reference to a national code

    Ref country code: DE

    Ref legal event code: R071

    Ref document number: 69320068

    Country of ref document: DE

    REG Reference to a national code

    Ref country code: DE

    Ref legal event code: R071

    Ref document number: 69320068

    Country of ref document: DE

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: DE

    Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

    Effective date: 20131203